Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method

Whereas the demand for missiles and rockets has exponentially augmented, but the difficulties related to the gas dynamics of these vehicles remains to be a threat. Whenever there is a sudden expansion, the pressure in the downstream is subatmospheric. This low pressure in the recirculation zone lea...

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Main Authors: Khan, Sher Afghan, Aabid, Abdul, Ghasi, Fharukh Ahmed Mehaboobali, Al-Robaian, Abdulrahman, Alsagri, Ali Sulaiman
Format: Article
Language:English
English
Published: Penerbit Akademia Baru 2019
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Online Access:http://irep.iium.edu.my/72294/1/72294_Analysis%20of%20Area%20Ratio%20In%20a%20CD%20Nozzle.pdf
http://irep.iium.edu.my/72294/7/72294_Analysis%20of%20area%20ratio%20in%20a%20CD%20nozzle_scopus.pdf
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http://www.akademiabaru.com/doc/CFDLV11_N5_P61_71.pdf
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spelling my.iium.irep.722942019-09-02T13:15:57Z http://irep.iium.edu.my/72294/ Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method Khan, Sher Afghan Aabid, Abdul Ghasi, Fharukh Ahmed Mehaboobali Al-Robaian, Abdulrahman Alsagri, Ali Sulaiman TL Motor vehicles. Aeronautics. Astronautics U Military Science (General) Whereas the demand for missiles and rockets has exponentially augmented, but the difficulties related to the gas dynamics of these vehicles remains to be a threat. Whenever there is a sudden expansion, the pressure in the downstream is subatmospheric. This low pressure in the recirculation zone leads to a considerable amount of drag, which is nearly two-thirds of the net drag of the aerospace vehicles. Hence, in view of the above problem, many researchers tried to control the base pressure depending upon the mission requirements. For example, in case of combustion chamber, we would like to decrease the base pressure as low as possible to have better mixing and efficient combustion, whereas, in case of the external ballistics application we would like to increase the base pressure as high as possible to reduce the drag of the projectiles to enhance the range. In this paper, investigated the effects of an area ratio in suddenly expanded duct and base pressure control with microjets using the computational fluid dynamics (CFD) method. A 1 mm orifice diameter of microjets placed at the pitch circle diameter (PCD) of 13 mm, located at 90 degrees for active control. The Mach number is M = 2.2, the L/D ratio is 8, the nozzle pressure ratio’s (NPR) is 9 and the area ratios are 2.56, 3.24, 4.86 and 6.25 considered in the present study. The design and modeling of convergent-divergent (CD) nozzle simulated using K-ε turbulence model for standard wall function. From the present results, it has been observed that the area ratio plays a crucial role in fixing the base pressure values. Penerbit Akademia Baru 2019-05-20 Article PeerReviewed application/pdf en http://irep.iium.edu.my/72294/1/72294_Analysis%20of%20Area%20Ratio%20In%20a%20CD%20Nozzle.pdf application/pdf en http://irep.iium.edu.my/72294/7/72294_Analysis%20of%20area%20ratio%20in%20a%20CD%20nozzle_scopus.pdf Khan, Sher Afghan and Aabid, Abdul and Ghasi, Fharukh Ahmed Mehaboobali and Al-Robaian, Abdulrahman and Alsagri, Ali Sulaiman (2019) Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method. CFD Letters, 11 (5). pp. 61-71. ISSN 2180-1363 http://www.akademiabaru.com/doc/CFDLV11_N5_P61_71.pdf
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
English
topic TL Motor vehicles. Aeronautics. Astronautics
U Military Science (General)
spellingShingle TL Motor vehicles. Aeronautics. Astronautics
U Military Science (General)
Khan, Sher Afghan
Aabid, Abdul
Ghasi, Fharukh Ahmed Mehaboobali
Al-Robaian, Abdulrahman
Alsagri, Ali Sulaiman
Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method
description Whereas the demand for missiles and rockets has exponentially augmented, but the difficulties related to the gas dynamics of these vehicles remains to be a threat. Whenever there is a sudden expansion, the pressure in the downstream is subatmospheric. This low pressure in the recirculation zone leads to a considerable amount of drag, which is nearly two-thirds of the net drag of the aerospace vehicles. Hence, in view of the above problem, many researchers tried to control the base pressure depending upon the mission requirements. For example, in case of combustion chamber, we would like to decrease the base pressure as low as possible to have better mixing and efficient combustion, whereas, in case of the external ballistics application we would like to increase the base pressure as high as possible to reduce the drag of the projectiles to enhance the range. In this paper, investigated the effects of an area ratio in suddenly expanded duct and base pressure control with microjets using the computational fluid dynamics (CFD) method. A 1 mm orifice diameter of microjets placed at the pitch circle diameter (PCD) of 13 mm, located at 90 degrees for active control. The Mach number is M = 2.2, the L/D ratio is 8, the nozzle pressure ratio’s (NPR) is 9 and the area ratios are 2.56, 3.24, 4.86 and 6.25 considered in the present study. The design and modeling of convergent-divergent (CD) nozzle simulated using K-ε turbulence model for standard wall function. From the present results, it has been observed that the area ratio plays a crucial role in fixing the base pressure values.
format Article
author Khan, Sher Afghan
Aabid, Abdul
Ghasi, Fharukh Ahmed Mehaboobali
Al-Robaian, Abdulrahman
Alsagri, Ali Sulaiman
author_facet Khan, Sher Afghan
Aabid, Abdul
Ghasi, Fharukh Ahmed Mehaboobali
Al-Robaian, Abdulrahman
Alsagri, Ali Sulaiman
author_sort Khan, Sher Afghan
title Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method
title_short Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method
title_full Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method
title_fullStr Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method
title_full_unstemmed Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method
title_sort analysis of area ratio in a cd nozzle with suddenly expanded duct using cfd method
publisher Penerbit Akademia Baru
publishDate 2019
url http://irep.iium.edu.my/72294/1/72294_Analysis%20of%20Area%20Ratio%20In%20a%20CD%20Nozzle.pdf
http://irep.iium.edu.my/72294/7/72294_Analysis%20of%20area%20ratio%20in%20a%20CD%20nozzle_scopus.pdf
http://irep.iium.edu.my/72294/
http://www.akademiabaru.com/doc/CFDLV11_N5_P61_71.pdf
_version_ 1646012438587375616
score 13.211869